• MIL D 8708 : C

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    DEMONSTRATION REQUIREMENTS FOR AIRPLANES

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Covers general requirements of NAVAIR (Naval Air Systems Command Headquarters) for the contractor demonstration of airplanes. Describes reporting requirements relating to demonstrations.

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Product Note NEW CHILD NOT 1 2019 IS NOW ADDED.<br>
    Publisher US Military Specs/Standards/Handbooks
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE AS 81366 : 2002 BOUNDARY LAYER CONTROL SYSTEM; PRESSURE
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL A 8866 : C AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
    MIL T 6396 : E TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
    MIL STD 7080 : 0 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    SAE ARP 217 D : 2016 TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
    MIL HDBK 244 : A GUIDE TO AIRCRAFT - STORES COMPATIBILITY
    MIL A 8865 : B AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
    MIL STD 1763 : A AIRCRAFT STORES CERTIFICATION PROCEDURES
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL A 8867 : C AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL A 8868 : B AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL D 23143 : A DATA, TECHNICAL AIRCRAFT, FOR DESIGN OF AVIATION TRAINING DEVICES
    MIL I 8670 : B INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    MIL W 006729 : B (1) WATERTIGHTNESS OF AIRCRAFT, TESTING
    MIL A 18717 : C ARRESTING HOOK INSTALLATIONS, AIRCRAFT
    MIL A 8861 : B AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    MIL HDBK 1763 : 0 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
    MIL STD 2072 : 0 SURVIVABILITY, AIRCRAFT, ESTABLISHMENT AND CONDUCT OF PROGRAMS FOR
    MIL F 8785 : C FLYING QUALITIES OF PILOTED AIRPLANES
    SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL T 5522 : D TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
    MIL I 6115 : A INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF
    DOD STD 2167 : A DEFENSE SYSTEM SOFTWARE DEVELOPMENT
    MIL B 83769 : D BATTERY, STORAGE, LEAD ACID, GENERAL SPECIFICATION FOR
    MIL F 15160 : G FUSE, INSTRUMENT, POWER, AND TELEPHONE, GENERAL SPECIFICATION FOR
    MIL F 8785 : C FLYING QUALITIES OF PILOTED AIRPLANES
    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL P 26366 : A PROPELLER SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
    DOD C 85050 : 0 CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL C 7762 : A COMPASS, INSTALLATION OF
    MIL A 8591 : H AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR
    MIL T 81571 : 0 THERMAL PROTECTIVE SYSTEM, AIRCRAFT COCKPIT, GENERAL SPECIFICATION FOR
    MIL STD 810 : G ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL E 85583 : A ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL P 26292 : C PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF
    MIL STD 1333 : B AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT
    MIL C 18244 : A CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL B 85110 : A BAR, REPEATABLE RELEASE HOLDBACK, AIRCRAFT LAUNCHING, GENERAL DESIGN REQUIREMENTS FOR
    MIL E 6051 : D ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    NISO Z39.18 : 1995 SCIENTIFIC AND TECHNICAL REPORTS - PREPARATION, PRESENTATION, AND PRESERVATION
    MIL STD 1760 : E AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    MIL D 6728 : A DAMPER, ENGINE EXHAUST FLAME AND GLARE
    MIL I 8675 : 0 INSTALLATION, AIRCRAFT ARMOR
    MIL C 23866 : A CONTROL SET, APPROACH POWER AN/ASN-54 (V)
    MIL E 7016 : F ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    MIL STD 470 : B MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL E 24021 : J NOTICE 1 ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT
    MIL C 83413 : A CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR
    MIL L 18276 : C LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF
    MIL I 8671 : D INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
    MIL D 19326 : H DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR
    DOD STD 2169 : 1985 HIGH ALTITUDE ELECTROMAGNETIC PULSE (HEMP) ENVIRONMENT (U) (CLASSIFIED)
    MIL E 18927 : E ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
    MIL S 18471 : G
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL STD 1388/1 : A LOGISTIC SUPPORT ANALYSIS
    MIL H 18325 : B HEATING AND VENTILATING SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL F 17874 : B FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
    MIL T 5842 : B TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR
    MIL L 22589 : D LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
    MIL STD 1757 : A LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE
    MIL L 85762 : A LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
    MIL E 5007 : D ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
    MIL STD 882 : E STANDARD PRACTICE FOR SYSTEM SAFETY
    MIL F 5372 : D FUSE, CURRENT LIMITER TYPE, AIRCRAFT
    MIL STD 461 : G REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MS 90298 : C CONNECTOR, RECEPTACLE ELECTRIC GROUNDING
    MIL A 8868 : B AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL C 8678 : 0 COOLING REQUIREMENTS OF POWER PLANT INSTALLATIONS
    MIL A 8867 : C AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL STD 471 : A MAINTAINABILITY DEMONSTRATION
    MIL B 8565 : J BATTERY AND CELL, STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL A 8861 : B AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    MIL F 23447 : 0 FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF
    MIL S 8512 : D SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    MIL STD 1472 : G HUMAN ENGINEERING
    MIL W 6729 : C WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL A 18717 : C ARRESTING HOOK INSTALLATIONS, AIRCRAFT
    MIL B 81757 : C BATTERIES & CELLS STORAGE, NICKEL CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR
    MIL T 18606 : 0 TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS
    MIL I 85071 : A INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR
    MIL R 23761 : B REGULATORS, VOLTAGE, AND CONTROL PANELS AIRCRAFT DIRECT CURRENT GENERATOR, GENERAL SPECIFICATION FOR
    MIL I 8670 : B INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT
    MIL B 5087 : B BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL W 5088 : L WIRING, AEROSPACE VEHICLE
    MIL I 8700 : A INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL STD 785 : B RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
    MIL E 7080 : B ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
    MIL A 19736 : A AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    MIL E 81910 : A ELECTRICAL POWER GENERATING AND CONTROL EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATIONS FOR
    MIL G 7940 : C GAGE, LIQUID QUANTITY, CAPACITOR TYPE, INSTALLATION AND CALIBRATION OF
    MIL C 5809 : G CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL STD 877 : 0 ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF
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